CASA C-212 Aviocar

Summary

Category	Transport aircraft
Origin country	🇪🇸 Spain
First flight	26 March 1971
Year of introduction	1974
Number produced	483 units

Description

The C-212 was developed during the 1960s by Construcciones Aeronáuticas SA (CASA) in response to the Spanish Air Force's need to replace its aging transport aircraft fleet. The aircraft was designed to perform a variety of military roles, including passenger transport, air medical services, and paratrooper duties, while also being suitable for civil operators. The first prototype of the C-212, a twin-engine 18-seat transport, conducted its maiden flight on 26 March 1971. In 1974, the Spanish Air Force purchased the C-212, which was then named Aviocar, to modernize its fleet. CASA subsequently developed a dedicated commercial version due to interest from several airlines. In 1997, the improved -400 model was introduced, featuring a glass cockpit and more powerful Honeywell TPE331 engines. Production of the type at the Seville facility continued for 40 years, with 485 aircraft produced there.

The CASA C-212 Aviocar is designed as a turboprop-powered STOL-capable cargo aircraft, characterized by its high-mounted wing, box-like fuselage, and conventional tail. It is specifically engineered to operate in austere conditions for extended durations without requiring substantial ground support. Its design incorporates features that provide STOL performance, such as rugged landing gear equipped with low-pressure tires, enabling operation from unpaved fields and in hot and high conditions. To enhance simplicity, the aircraft is fitted with non-retractable tricycle undercarriage. Depending on configuration, the cabin can accommodate between 21 and 28 passengers; in a paratroop configuration, it can accommodate up to 24 paratroopers plus a jumpmaster on foldable sidewall seats, while a mixed configuration allows for up to ten soldiers and a single vehicle. The absence of a pressurized fuselage restricts the C-212 to relatively low-altitude flights below 10,000 feet (3,000 meters), making it suitable for short-range regional airline services.

The CASA C-212 can be outfitted with up to 500 kg (1,102 lb) of weaponry on two hardpoints. This capacity typically accommodates machine gun pods or rocket launchers, enabling the aircraft to support tactical missions such as close air support or armed reconnaissance.

By 2013, 290 C-212s were flying in 40 countries, with Indonesia as the primary operator with 70 aircraft. The C-212 has been widely used both as a commuter airliner and as a military platform, employed by charter and short-haul aviation companies and numerous national air forces, and is commonly used in transport, surveillance, and search and rescue roles. The U.S. Army Special Operations Command has operated the C-212, designated C-41A, for troop infiltration and exfiltration, supply drops, and airborne operations. Additional aircraft were operated by private military contractor Blackwater during the Iraq War and the War in Afghanistan for supply drops to US ground forces in remote areas. Australian airline Skytraders has supported Australia’s scientific research assets across Antarctica and the Southern Ocean with the type.

Main Variants:

C-212A: The original military production version, also known as the C-212-5, C-212-5 series 100M, and designated as T-12B and D-3A (for medevac aircraft) by the Spanish Air Force.
C-212C: The initial civil version of the C-212, aimed at commercial operators.
C-212 series 200M: This military version, designated T-12D in Spanish service and Tp 89 for the Swedish Air Force, has also been adapted into specialized ASW and maritime patrol aircraft.
C-212 series 300 airliner: A 26-seat regional airliner configuration, expanding the C-212's role in civilian transport.
C-212-400: An upgraded variant featuring more powerful engines, an increased payload, and enhanced avionics relocated to the nose.

Technical specifications

Version: C-212-300M
Maximum speed	370 km/h (230 mph)
Wing area	41 m² (441.3 sqft)
Wingspan	20.3 m (66.5 ft)
Height	6.3 m (20.7 ft)
Length	16.2 m (53.1 ft)
Service ceiling	7925 m (26001 ft)
Empty weight	3780 kg (8333 lbs)
Max. takeoff weight	7700 kg (16976 lbs)
Climb rate	8.3 m/s (27.2 ft/s)
Powerplant	2 × turboprops Garrett TPE331-10R-513C delivering 671 kW

Current operating countries

Country		Units
	Indonesia	35 (+3)
	Spain	11
	Zimbabwe	9
	Colombia	7
	Mexico	7
	Chile	5
	United States	5
	Uruguay	5
	Venezuela	5
	Argentina	3
	Botswana	3
	Dominican Republic	3
	Panama	3
	Paraguay	3
	South Africa	3
	Vietnam	3
	Angola	2
	Lesotho	2
	Philippines	2
	Thailand	2
	Ecuador	1
	Senegal	0 (+2)